KR101234831B1 - 진동 댐퍼 기구, 캐리어 구조체를 포함하는 항공기 및 이러한 기구를 구비한 회전자 - Google Patents
진동 댐퍼 기구, 캐리어 구조체를 포함하는 항공기 및 이러한 기구를 구비한 회전자 Download PDFInfo
- Publication number
- KR101234831B1 KR101234831B1 KR1020100128436A KR20100128436A KR101234831B1 KR 101234831 B1 KR101234831 B1 KR 101234831B1 KR 1020100128436 A KR1020100128436 A KR 1020100128436A KR 20100128436 A KR20100128436 A KR 20100128436A KR 101234831 B1 KR101234831 B1 KR 101234831B1
- Authority
- KR
- South Korea
- Prior art keywords
- resonator
- support
- rotor
- vibration
- carrier structure
- Prior art date
Links
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/001—Vibration damping devices
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/10—Suppression of vibrations in rotating systems by making use of members moving with the system
- F16F15/14—Suppression of vibrations in rotating systems by making use of members moving with the system using masses freely rotating with the system, i.e. uninvolved in transmitting driveline torque, e.g. rotative dynamic dampers
- F16F15/1407—Suppression of vibrations in rotating systems by making use of members moving with the system using masses freely rotating with the system, i.e. uninvolved in transmitting driveline torque, e.g. rotative dynamic dampers the rotation being limited with respect to the driving means
- F16F15/1464—Masses connected to driveline by a kinematic mechanism or gear system
- F16F15/1471—Masses connected to driveline by a kinematic mechanism or gear system with a kinematic mechanism, i.e. linkages, levers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/001—Vibration damping devices
- B64C2027/005—Vibration damping devices using suspended masses
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Vibration Prevention Devices (AREA)
- Fluid-Damping Devices (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Support Of Aerials (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0906121A FR2954274B1 (fr) | 2009-12-17 | 2009-12-17 | Mecanisme amortisseur de vibrations, et appareil volant muni d'une structure porteuse et d'un rotor muni d'un tel mecanisme |
FR0906121 | 2009-12-17 |
Publications (2)
Publication Number | Publication Date |
---|---|
KR20110069721A KR20110069721A (ko) | 2011-06-23 |
KR101234831B1 true KR101234831B1 (ko) | 2013-02-19 |
Family
ID=42320865
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
KR1020100128436A KR101234831B1 (ko) | 2009-12-17 | 2010-12-15 | 진동 댐퍼 기구, 캐리어 구조체를 포함하는 항공기 및 이러한 기구를 구비한 회전자 |
Country Status (6)
Country | Link |
---|---|
US (1) | US8695917B2 (fr) |
EP (1) | EP2340997B1 (fr) |
KR (1) | KR101234831B1 (fr) |
CN (1) | CN102102733B (fr) |
AT (1) | ATE556927T1 (fr) |
FR (1) | FR2954274B1 (fr) |
Families Citing this family (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP5022457B2 (ja) * | 2010-02-17 | 2012-09-12 | 三菱重工業株式会社 | 振動低減装置および振動低減方法 |
GB2482545B (en) * | 2010-08-06 | 2017-05-03 | Ge Aviat Systems Ltd | Aircraft propellers with composite blades mounted to a single propeller hub |
KR101752645B1 (ko) | 2011-02-04 | 2017-06-30 | 로오드 코포레이션 | 공진 관성형 액추에이터를 구비한 회전익 항공기 진동 제어 시스템 |
US9126680B2 (en) * | 2011-11-16 | 2015-09-08 | Textron Innovations Inc. | Dual mode rotor hub assembly |
US9260185B2 (en) * | 2012-01-25 | 2016-02-16 | Textron Innovations Inc. | System and method of harvesting power with a rotor hub damper |
JP5863528B2 (ja) * | 2012-03-23 | 2016-02-16 | 三菱重工業株式会社 | 振動低減装置 |
WO2015109089A1 (fr) * | 2014-01-15 | 2015-07-23 | Lord Corporation | Systèmes, dispositifs et procédés de commande de vibration active basés sur un moyeu et comportant des rotors non équilibrés et décalés |
US10065730B2 (en) | 2014-01-22 | 2018-09-04 | Bell Helicopter Textron Inc. | Active vibration control system with non-concentric revolving masses |
FR3019522B1 (fr) * | 2014-04-07 | 2016-05-20 | Airbus Helicopters | Ensemble sustentateur amovible d'un giravion et giravion |
US10513330B2 (en) | 2014-10-03 | 2019-12-24 | Sikorsky Aircraft Corporation | Blade damper with a magnetic contaminants trap |
US9788446B1 (en) * | 2015-03-27 | 2017-10-10 | Paul H. Townsend | Mobile vibration isolation device |
US9399380B1 (en) * | 2015-04-17 | 2016-07-26 | Ping Fan | Vibration-type electric generator applied to automobile suspension system |
US9828084B2 (en) * | 2015-05-06 | 2017-11-28 | The Boeing Company | Vibration dampening for horizontal stabilizers |
US10507920B2 (en) * | 2015-05-18 | 2019-12-17 | Sikorsky Aircraft Corp. | Systems and methods for lifting body vibration control |
CN205186541U (zh) * | 2015-11-24 | 2016-04-27 | 零度智控(北京)智能科技有限公司 | 无人机机体支架 |
CN106741926A (zh) * | 2015-11-24 | 2017-05-31 | 中国直升机设计研究所 | 一种直升机球柔性桨毂阻尼器布置形式 |
US10457388B2 (en) * | 2016-02-16 | 2019-10-29 | Bell Helicopter Textron, Inc. | Rotor assembly with high lock-number blades |
US10472057B2 (en) * | 2016-02-16 | 2019-11-12 | Bell Helicopter Textron Inc. | Rotor assembly with high lock-number blades |
FR3052209B1 (fr) * | 2016-06-02 | 2018-06-01 | Airbus Helicopters | Resonateur, et aeronef muni de ce resonateur |
FR3053312B1 (fr) * | 2016-06-29 | 2019-07-19 | Airbus Helicopters | Rotor et aeronef pourvu d'un tel rotor |
US10773798B2 (en) * | 2017-09-29 | 2020-09-15 | Bell Textron Inc. | Rotor hub with blade-to-blade dampers attached to the pitch change axis |
US10746047B2 (en) | 2017-10-27 | 2020-08-18 | General Electric Company | Structure for mitigating vibratory modes of counter-rotating engine rotors |
US10597150B2 (en) * | 2018-04-24 | 2020-03-24 | Textron Innovations Inc. | Articulated rotor systems with blade-to-blade damping |
WO2019217532A1 (fr) * | 2018-05-08 | 2019-11-14 | Avx Aircraft Company | Moyeu de rotor |
US20220144416A1 (en) * | 2020-11-08 | 2022-05-12 | Bell Textron Inc. | Liquid inertia vibration elimination system with compound period strut |
US11428160B2 (en) | 2020-12-31 | 2022-08-30 | General Electric Company | Gas turbine engine with interdigitated turbine and gear assembly |
CN113353251B (zh) * | 2021-08-09 | 2021-12-28 | 四川聚变未来航空科技有限公司 | 一种多旋翼飞行器 |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5431261A (en) * | 1994-05-12 | 1995-07-11 | University Of Connecticut | Delayed resonators as active dynamic absorbers |
US5934424A (en) * | 1996-11-01 | 1999-08-10 | The University Of Connecticut | Centrifugal delayed resonator pendulum absorber |
FR2808256A1 (fr) * | 2000-04-27 | 2001-11-02 | Eurocopter France | Rotor avec antivibreur de tete a pendules verticaux |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3484173A (en) * | 1968-12-06 | 1969-12-16 | United Aircraft Corp | Double action damper bumper |
FR2630703B1 (fr) * | 1988-04-29 | 1990-08-24 | Aerospatiale | Tete de rotor de giravion a tirants interpales de rappel elastique avec amortissement incorpore |
FR2653405B1 (fr) * | 1989-10-20 | 1992-02-07 | Aerospatiale | Dispositif visco-elastique rotatif de rappel elastique et d'amortissement en trainee pour pale de rotor de giravion, et tete de rotor le comportant. |
FR2733961B1 (fr) * | 1995-05-12 | 1997-07-18 | Eurocopter France | Dispositif d'amortissement de trainee des pales d'un rotor |
FR2750948B1 (fr) * | 1996-07-12 | 1998-10-30 | Eurocopter France | Dispositif de blocage, au moins en pas, des pales d'un rotor |
FR2768995B1 (fr) * | 1997-10-01 | 1999-12-03 | Eurocopter France | Resonateur pendulaire de tete de rotor |
FR2784350B1 (fr) | 1998-10-12 | 2000-12-08 | Eurocopter France | Dispositif pour reduire des vibrations engendrees sur la structure d'un aeronef a voilure tournante |
FR2826933B1 (fr) * | 2001-07-04 | 2003-09-26 | Eurocopter France | Amortisseur de trainee a inertie fluide pour rotor de giravion |
FR2835506B1 (fr) * | 2002-02-06 | 2004-03-12 | Eurocopter France | Amortisseur de trainee a double piston pour rotor de giravion |
FR2837462B1 (fr) * | 2002-03-20 | 2004-05-28 | Eurocopter France | Rotor de giravion a entrainement homocinetique |
FR2890937B1 (fr) * | 2005-09-21 | 2009-04-24 | Eurocopter France | Rotor de giravion a pales articulees en battement et en trainee |
FR2910877B1 (fr) * | 2006-12-28 | 2009-09-25 | Eurocopter France | Amelioration aux rotors de giravions equipes d'amortisseurs interpales |
EP2184229B1 (fr) * | 2008-11-11 | 2012-10-17 | AGUSTAWESTLAND S.p.A. | Rotor d'hélicoptère |
-
2009
- 2009-12-17 FR FR0906121A patent/FR2954274B1/fr active Active
-
2010
- 2010-12-01 EP EP10015170A patent/EP2340997B1/fr active Active
- 2010-12-01 AT AT10015170T patent/ATE556927T1/de active
- 2010-12-15 KR KR1020100128436A patent/KR101234831B1/ko active IP Right Grant
- 2010-12-15 US US12/968,653 patent/US8695917B2/en active Active
- 2010-12-15 CN CN201010604120.4A patent/CN102102733B/zh active Active
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5431261A (en) * | 1994-05-12 | 1995-07-11 | University Of Connecticut | Delayed resonators as active dynamic absorbers |
US5934424A (en) * | 1996-11-01 | 1999-08-10 | The University Of Connecticut | Centrifugal delayed resonator pendulum absorber |
FR2808256A1 (fr) * | 2000-04-27 | 2001-11-02 | Eurocopter France | Rotor avec antivibreur de tete a pendules verticaux |
US6494680B2 (en) * | 2000-04-27 | 2002-12-17 | Eurocopter | Rotor with rotor head vibration suppressor comprising vertical pendulums |
Also Published As
Publication number | Publication date |
---|---|
FR2954274A1 (fr) | 2011-06-24 |
EP2340997B1 (fr) | 2012-05-09 |
EP2340997A1 (fr) | 2011-07-06 |
ATE556927T1 (de) | 2012-05-15 |
FR2954274B1 (fr) | 2012-02-24 |
US20110155841A1 (en) | 2011-06-30 |
CN102102733A (zh) | 2011-06-22 |
KR20110069721A (ko) | 2011-06-23 |
CN102102733B (zh) | 2013-08-21 |
US8695917B2 (en) | 2014-04-15 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
KR101234831B1 (ko) | 진동 댐퍼 기구, 캐리어 구조체를 포함하는 항공기 및 이러한 기구를 구비한 회전자 | |
CN101674982B (zh) | 旋翼浆毂振动衰减器 | |
US11884385B2 (en) | Active vibration control system with non-concentric revolving masses | |
US8474745B2 (en) | Rotor hub vibration attenuator | |
KR101281162B1 (ko) | 플랩과 래그에 힌지식으로 연결된 블레이드를 갖는 회전익항공기의 로터 | |
US11767105B2 (en) | Mount for supporting a component and attenuating noise | |
JP2015071410A (ja) | 振動減衰装置を備える回転翼航空機回転翼 | |
US8820674B2 (en) | Rotor carrier structure with a damper device for avoiding unstable coupling between resonant vibration modes | |
US8573935B2 (en) | Helicopter rotor comprising a vibration damper, and method for updating the same | |
EP3194264B1 (fr) | Système d'actionnement d'aéronef produisant une charge anti-vibrations | |
JPH0159158B2 (fr) | ||
JP2002500119A (ja) | 回転翼機用の防振装置 | |
KR101227106B1 (ko) | 블레이드 댐퍼, 및 이런 댐퍼를 구비한 로터 | |
KR101425482B1 (ko) | 회전익 항공기의 메인 로터 유닛에 관한 리드 래그 댐퍼 | |
Riemenschneider et al. | Additional applications of active twist blades | |
Cassier | Experimentation of Triflex rotor head on Gazelle helicopter | |
JPH03258692A (ja) | 回転翼機振動低減装置 |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
A201 | Request for examination | ||
E902 | Notification of reason for refusal | ||
E701 | Decision to grant or registration of patent right | ||
GRNT | Written decision to grant | ||
FPAY | Annual fee payment |
Payment date: 20160204 Year of fee payment: 4 |
|
FPAY | Annual fee payment |
Payment date: 20170202 Year of fee payment: 5 |
|
FPAY | Annual fee payment |
Payment date: 20180201 Year of fee payment: 6 |
|
FPAY | Annual fee payment |
Payment date: 20190131 Year of fee payment: 7 |